› › Robust Adaptive Control Of Rigid Spacecraft Attitude Maneuvers




Fast Satellite Attitude Maneuver and Control

Author : Dong Ye

Publisher : Academic Press

Page : 280 pages

File Size : 19,77 MB

Release : 2022-08-02

Category : Technology & Engineering

ISBN : 0323954561

Get eBook

Book Description

Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems. Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches Contains comprehensive, up-to-date references, which play an indicative role for further study



Spacecraft Attitude Control

Author : Chuang Liu

Publisher : Elsevier

Page : 386 pages

File Size : 44,26 MB

Release : 2022-01-31

Category : Science

ISBN : 0323990061

Get eBook

Book Description

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problemsfor spacecraft attitude control systems using convex optimization and, specifi cally,through a linear matrix inequality (LMI) approach. High-precision pointing and improvedrobustness in the face of external disturbances and other uncertainties are requirementsfor the current generation of spacecraft. This book presents an LMI approach to spacecraftattitude control and shows that all uncertainties in the maneuvering process can besolved numerically. It explains how a model-like state space can be developed through amathematical presentation of attitude control systems, allowing the controller in question tobe applied universally. The authors describe a wide variety of novel and robust controllers,applicable both to spacecraft attitude control and easily extendable to second-ordersystems. Spacecraft Attitude Control provides its readers with an accessible introductionto spacecraft attitude control and robust systems, giving an extensive survey of currentresearch and helping researchers improve robust control performance. Considers the control requirements of modern spacecraft Presents rigid and flexible spacecraft control systems with inherent uncertainties mathematically, leading to a model-like state space Develops a variety of novel and robust controllers directly applicable to spacecraft control as well as extendable to other second-order systems Includes a systematic survey of recent research in spacecraft attitude control



Fault-Tolerant Attitude Control of Spacecraft

Author : Qinglei Hu

Publisher : Elsevier

Page : 306 pages

File Size : 28,41 MB

Release : 2021-06-09

Category : Technology & Engineering

ISBN : 0323901247

Get eBook

Book Description

Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour. Finally, the book looks at the future of this interesting topic, offering readers a one-stop solution for those working on fault-tolerant attitude control for spacecraft. Presents the fundamentals of fault-tolerant attitude control systems for spacecraft in one practical solution Gives the latest research and thinking on nonlinear attitude control, fault tolerant control, and reliable attitude control Brings together concepts in fault control theory, fault diagnosis, and attitude control for spacecraft Covers advances in theory, technological aspects, and applications in spacecraft Presents detailed numerical and simulation results to assist engineers Offers a clear, systematic reference on fault-tolerant control and attitude control for spacecraft



Robust Adaptive and Fault-tolerant Control for Attitude Tracking of Spacecraft

Author : Wenchuan Cai

Publisher :

Page : 230 pages

File Size : 24,48 MB

Release : 2010

Category : Adaptive control systems

ISBN :

Get eBook

Book Description

Explores an indirect (non-regressor based) adaptive and robust algorithm to deal with the effects of system uncertainties, unexpected disturbances, subsystem failures, and limited resources. Develops a robust adaptive attitude control scheme, based on the indirect adaptive algorithm, which was verified to be robust against external disturbances and adaptive to unknown and time-varying mass/inertia properties, and to tolerate limited thrusts. Designs three robust adaptive and fault-tolerant attitude control laws to accommodate actuator failures by extending the idea of the robust adaptive control method.







Intelligent Autonomous Control of Spacecraft with Multiple Constraints

Author : Qinglei Hu

Publisher : Springer Nature

Page : 346 pages

File Size : 44,88 MB

Release : 2023-05-02

Category : Technology & Engineering

ISBN : 9819906814

Get eBook

Book Description

This book explores the intelligent autonomous control problems for spacecraft with multiple constraints, such as pointing/path constraints, linear/angular velocity constraints, performance constraints, etc. It provides an almost self-contained presentation of dynamics modeling, controller design and analysis, as well as simulation studies. The book aims to offer a valuable guide for researchers and aerospace engineers to address the theoretical and technical difficulties in different applications, ranging from spacecraft attitude reorientation and tracking to spacecraft proximity operations, and is mainly intended for technical and engineering staff engaged in spacecraft dyanmics and control areas.



Fundamentals of Spacecraft Attitude Determination and Control

Author : F. Landis Markley

Publisher : Springer

Page : 486 pages

File Size : 48,68 MB

Release : 2014-05-31

Category : Technology & Engineering

ISBN : 1493908022

Get eBook

Book Description

This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice and also provides prototype algorithms that are readily available on the author’s website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website.